US20180117512A1 - Multiple Stage Rotating Coalescer Devices - Google Patents
Multiple Stage Rotating Coalescer Devices Download PDFInfo
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- US20180117512A1 US20180117512A1 US15/561,170 US201515561170A US2018117512A1 US 20180117512 A1 US20180117512 A1 US 20180117512A1 US 201515561170 A US201515561170 A US 201515561170A US 2018117512 A1 US2018117512 A1 US 2018117512A1
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- rotating
- stage
- coalescing
- coalescer
- media
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
- B01D46/0027—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours with additional separating or treating functions
- B01D46/003—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours with additional separating or treating functions including coalescing means for the separation of liquid
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D45/00—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces
- B01D45/12—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by centrifugal forces
- B01D45/14—Separating dispersed particles from gases or vapours by gravity, inertia, or centrifugal forces by centrifugal forces generated by rotating vanes, discs, drums or brushes
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
- B01D46/0052—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours with filtering elements moving during filtering operation
- B01D46/0056—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours with filtering elements moving during filtering operation with rotational movement
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M13/00—Crankcase ventilating or breathing
- F01M13/04—Crankcase ventilating or breathing having means for purifying air before leaving crankcase, e.g. removing oil
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D2279/00—Filters adapted for separating dispersed particles from gases or vapours specially modified for specific uses
- B01D2279/30—Filters adapted for separating dispersed particles from gases or vapours specially modified for specific uses for treatment of exhaust gases from IC Engines
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L67/00—Compositions of polyesters obtained by reactions forming a carboxylic ester link in the main chain; Compositions of derivatives of such polymers
- C08L67/04—Polyesters derived from hydroxycarboxylic acids, e.g. lactones
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M13/00—Crankcase ventilating or breathing
- F01M13/04—Crankcase ventilating or breathing having means for purifying air before leaving crankcase, e.g. removing oil
- F01M2013/0422—Separating oil and gas with a centrifuge device
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M13/00—Crankcase ventilating or breathing
- F01M13/04—Crankcase ventilating or breathing having means for purifying air before leaving crankcase, e.g. removing oil
- F01M2013/0438—Crankcase ventilating or breathing having means for purifying air before leaving crankcase, e.g. removing oil with a filter
Definitions
- the field of the invention relates to coalescing devices.
- the field of the invention relates to coalescing devices comprising multiple rotating separation elements.
- Rotating coalescers are utilized in crankcase ventilation (CV) systems for removing oil from crankcase blow-by gases.
- the blow-by gases enter the rotating coalescer device axially at the center of the device.
- the gases are turned 90 degrees, pass through a rotating coalescer section, and exit radially from the outer face of the rotating coalescer device.
- the rotating coalescer device itself is in the form of a ring and the space in the middle of the ring is either left open or optionally includes radial vanes which facilitate flow through the device.
- Rotating coalescers may include fibrous filters as well as centrifugal separation devices. Performance attributes of rotating coalescer devices may be measured in terms of pressure drop (or rise) through the device and efficiency of oil removal.
- the oil droplets e.g., aerosol
- the centrifugal force removes the larger drops by overcoming the surface drag force of the media fibers.
- This aspect increases the coalescence of the oil from the coalescer by providing improved drainage compared to a stationary coalescer.
- the improved drainage from the rotating coalescing filter aids in improving the filtration efficiency as well as greatly reducing the pressure drop across the filter.
- One stage of the device is a rotating coalescer element.
- the devices may include an additional separation element, either upstream or downstream of the rotating coalescer element, which may include a cone stack separator or an additional rotating coalescer element.
- the multiple stage rotating coalescer device includes a first stage including a rotating coalescing element.
- the rotating coalescing element includes coalescing media.
- the device includes a second stage.
- the second stage is either upstream or downstream of the first stage.
- the second stage includes one of a rotating cone stack separator or a separate rotating coalescing element having coalescing media.
- the system includes a housing having an inlet and an outlet.
- the inlet is configured to receive blow-by gas from a crankcase of an internal combustion engine.
- the outlet is configured to output filtered air.
- the system further includes a rotating coalescer positioned within the housing.
- the rotating coalescer includes a first endplate and a second endplate.
- a spiral vane preseparator is positioned between the first endplate and the second endplate.
- the spiral vane preseparator includes a plurality of curved vanes that cause separation of an oil from the blow-by gas and pumping of the blow-by gas when the spiral vane preseparator is rotating.
- the rotating coalescer further includes a coalescer element circumferentially surrounding the spiral vane preseparator and positioned between the first endplate and the second endplate.
- the coalescer element is comprised of coalescer media.
- the rotating coalescer includes a de-swirler coupled to the first endplate opposite the spiral vane preseparator and the coalescer element.
- FIG. 1 is a cross-sectional view of a rotating coalescer device according to an exemplary embodiment.
- FIG. 2 is a close-up cross-sectional view of the coalescer device of FIG. 1 .
- FIG. 3 is a cross-sectional view of a rotating coalescing device according to another exemplary embodiment.
- FIG. 4 is a cross-sectional view of a rotating coalescer device according to still another exemplary embodiment.
- FIG. 5 is a cross-sectional view of a rotating coalescer device according to a further exemplary embodiment.
- FIG. 6 is a cross-sectional view of a rotating coalescer device according to yet another exemplary embodiment.
- FIG. 7 is a cross-sectional perspective view of a rotating coalescer according to an exemplary embodiment.
- FIGS. 8 and 9 are cross-sectional views of the endplates of the rotating coalescer of FIG. 7 .
- FIG. 10 is a cross-sectional view of the rotating coalescer of FIG. 7 fitted within a housing and having a de-swirler attached.
- FIG. 11 is a cross-sectional view showing the de-swirler of FIG. 10 .
- the presently disclosed devices may include an integrated coalescing element upstream or downstream of a cone stack centrifugal separator in order to improve efficiency and pumping power of the devices.
- the devices may include two stages of aerosol separation (e.g., for rotating-type separators).
- the presently disclosed devices also may include a shroud that collects and drains collected oil from the interstitial space between the cone stack separator and the coalescing element.
- the devices may integrate a cone stack separator downstream of a coalescing element in an outside-in configuration in order to improve overall performance and better accommodate the air/oil flow through the device.
- the disclosed devices may include a secondary rotating coalescer element downstream of a primary rotating coalescer element, where flow through the primary rotating element is inside-out and flow through the secondary rotating element is outside-in.
- the two rotating elements may share the same base plate.
- the primary and secondary elements rotate on single-drive or multiple-drive mechanisms that utilize single or multiple shafts and have multiple seals.
- the rotation of the primary and secondary element in the presently disclosed devices may provide continuous self-cleaning of the media of the elements and enhanced droplet coalescing.
- the fiber architecture of the media of the primary and secondary elements may be the same or different and optionally may include oleophobic treatment.
- the media of the secondary element may be an oleophobic screen that prevents oil carryover and increases the pumping effect of the device.
- the coalescer device 100 includes a centrifugal cone stack separator 102 positioned in the center of the coalescer device 100 .
- the cone stack separator 102 acts as a pre-cleaner, providing an initial stage of inertial separation of aerosol (e.g., oil) from blow-by gases entering the inlet 104 prior to the blow-by gases passing through the coalescing element 106 .
- the coalescing element 106 is comprised of a coalescing media.
- the coalescing element 106 is a second stage of separation of aerosol from the blow-by gases.
- the pre-cleaning reduces the total amount of oil that the coalescing element 106 needs to separate by pre-capturing some fraction of the overall oil aerosol contained in the crankcase blow-by gases.
- the cone stack separator 102 also increases the amount of pumping of the blow-by gas flow in the coalescer device 100 .
- the cone stack separator 102 also helps to distribute the flow evenly across the inlet face of the coalescing element 106 thereby increasing the performance of the coalescing element 106 .
- both the cone stack separator 102 and the coalescing element 106 are coupled to and rotated by a shaft 108 passing through the center of the coalescer device 100 .
- the shaft 108 is hollow and provides the inlet into the coalescer device 100 .
- the blow-by gas flow enters the center of a housing 110 of the device 100 , into the inside of the cone stack separator 102 via the inlet 104 .
- blow-by gas flows radially outward where at least some of the aerosol in the blow-by gas is removed due to centrifugal impaction of the aerosol on the surfaces of the cone stack separator 102 .
- the cone stack separator 102 further adds mechanical energy to the blow-by gas flow by accelerating the flow of the blow-by gas in a tangential direction with respect to the center axis of the coalescer device 100 .
- the added mechanical energy to the blow-by gas by the cone stack separator 102 creates a pumping effect similar to the action of a pump, which reduces the pressure drop caused by the coalescer device 100 .
- the blow-by gas flow After exiting from the cone stack separator 102 , the blow-by gas flow enters the coalescing element 106 where additional filtration (e.g., coalescing of the aerosol in the blow-by gas) and pumping takes place.
- blow-by flow is vented either to the atmosphere (e.g., as done in an open CV system) or back to an intake stream (e.g., to the turbocharger inlet) of the internal combustion engine for combustion (e.g., as done in a closed CV system).
- FIG. 2 a close-up cross-sectional view of the coalescer device 100 is shown.
- FIG. 2 shows the flow of the blow-by gas passing through the cone stack separator 102 and through the coalescing element 106 .
- the cone stack separator 102 is comprised of a plurality of cones 202 .
- the cones 202 are spaced out to provide a plurality of flow paths in between pairs of adjacent cones 202 .
- Each of the cones 202 includes a bend that causes the centrifugal impaction of the aerosol on the surfaces of the cone stack separator 102 as discussed above.
- FIG. 3 shows a cross-sectional view of a coalescer device 300 is shown according to an exemplary embodiment.
- the coalescer device 300 is a rotating coalescer device. Similar to the coalescer device 100 , the coalescer device 300 includes a cone stack separator 302 and a coalescing element 304 comprised of coalescing media. The cone stack separator 302 and the coalescing media are housed within a housing 306 . During operation, the cone stack separator 302 and the coalescing element 304 are rotated about a central axis 308 in a similar manner as described above with respect to the coalescer device 100 .
- the coalescer device 300 separates oil 310 from a flow 312 of blow-by gases containing aerosol.
- the cones 314 of the cone stack separator include spacers (e.g., raised ridges, ribs, dots, etc.) that radiate out in a straight line or a curve. These spacers provide separation between the cones 314 .
- the coalescer device 300 includes a shroud 316 that collects oil 310 exiting from the cone stack separator 302 . The collected oil 310 falls down the face of the shroud to the bottom of the rotating module 318 due to gravity.
- the rotating module 318 houses cone stack separator 302 and the coalescing element 304 for rotation within the housing 306 .
- the open area below the shroud 316 leading to the coalescer element 304 is arranged such that the collected oil 310 is not carried over to the coalescer element 304 and instead collects at the bottom of the rotating module 318 where it drains through a preseparator drain 320 .
- the preseparator drain 320 rotates with the rotating module 318 .
- the preseparator drain 320 is sized and positioned based on the pressure difference on either side of the rotating module 318 to allow for draining of the separated oil 310 via gravity.
- the dimensions of the preseparator drain 320 are selected in order to minimize the potential for blow-by gas flow from the cone stack separator 302 to bypass the coalescer element 304 by flowing out of the preseparator drain 320 .
- the size of the preseparator drain 320 is also sized based at least in part on the pumping force generated by the cone stack separator 302 . Separated oil 310 does not flow back through the inlet because the rotating module 318 is sealed against the housing 310 through at least one seal 322 (shown as two seals). Oil 310 separated via the cone stack separator 302 and the coalescer element 304 is drained from the housing via a housing drain 324 .
- FIG. 4 shows a cross-sectional view of a coalescing device 400 according to an exemplary embodiment.
- the coalescing device 400 includes a cone stack separator 402 , which functions as an inertial post-separator, and a rotating coalescer element 404 comprised of coalescing media.
- the cone stack separator 402 functions as an inertial post-separator because the cone stack separator 402 is positioned downstream of the rotating coalescer element 404 with respect to the by-pass gas flow 406 .
- the cone stack separator 402 and the coalescing element 404 are rotated in a similar manner as described above with respect to devices 100 and 300 to effect pumping and separation of oil from the by-pass gas flow 406 .
- coalescing device 400 a top portion of the coalescing element opposite the inlet 408 is received in a bottom portion of the cone stack separator 402 , which is utilized for guiding oil 410 to the drain 412 of the housing 414 .
- slots or holes may be provided to improve drainage and prevent oil carryover.
- FIG. 5 shows a cross-sectional view of a rotating coalescer device 500 according to another exemplary embodiment.
- the rotating coalescer device 500 includes a cone stack separator 502 placed downstream of a coalescer element 504 in an inside-out flow configuration.
- the coalescer device 500 of FIG. 5 is designed to reduce oil carryover and to separate out re-entrained droplets.
- the coalescer device 500 may be particularly desirable for coalescers having a housing that is diametrically constrained (e.g., due to limited space on an engine-mounted device), where oil carryover is particularly an issue.
- the post-separator cone stack separator 502 has inside-out flow and the re-entrained oil is flung from the device due to centrifugal force. Separated oil drains from the housing 506 through a drain 508 .
- the cone stack separator 502 is shaped to direct the flow of blow-by gas towards the drain 508 .
- the cone stack separator 502 includes slots or holes 510 to drain the coalesced droplets by gravitational force and by positive pumping pressure created through the rotation of the coalescer element 504 and the cone stack separator 502 .
- the media of the coalescer element 504 may be embedded or coupled to the cone stack separator 502 .
- the rotating coalescer device 600 includes a primary rotating coalescing element 602 and a downstream, secondary rotating coalescing element 604 . Both the primary and secondary rotating coalescing elements 602 and 604 rotate to effect separation of oil from and pumping of blow-by gas passing through the rotating coalescer device 600 . Both the primary and secondary rotating coalescing elements 602 and 604 are comprised of filter media.
- the secondary element 604 can be comprised of either similar filter media material or another type of media material as the primary coalescing element 602 .
- the two coalescing elements 602 and 604 are separated by a barrier 606 positioned between the two elements 602 and 604 .
- the barrier 606 ensures that by-pass gas flows first through the primary coalescing element 602 (in an inside-out flow pattern) and then through the secondary coalescing element 604 (in an outside-in flow pattern).
- the barrier 606 ensures that the by-pass gases flowing through the two coalescing elements 602 and 604 do not mix.
- the primary and secondary coalescing elements 602 and 604 are rotated with either a single or multiple shafts driven by a single drive mechanism or multiple drive mechanisms.
- the by-pass flow enters through the inlet 608 on the upstream side and then exits radially out of the primary coalescing element 602 .
- the secondary coalescing element 604 captures any re-entrained oil droplets and excessive oil that gets carried over rendering the air flow on the downstream side completely oil free.
- the secondary coalescing element 604 will eliminate any carryover oil that has not previously drained from the device. Any further carryover oil has to overcome the centrifugal force created by the rotating secondary element. Clean air passes out of the housing 610 through an outlet 612 . Separated oil exits the housing through a drain 614 .
- FIG. 7 a cross-sectional perspective view of a rotating coalescer 700 is shown according to still another exemplary embodiment.
- the rotating coalescer 700 separates oil from blow-by gas entering the rotating coalescer 700 through a central inlet 702 .
- the rotating coalescer 700 is a two-stage coalescer.
- the blow-by gas is first routed from the central inlet 702 through a spiral vane preseparator 704 in an inside-out flow direction. After passing through the spiral vane preseparator 704 , the blow-by gas is routed through a coalescer element 706 .
- the coalescer element 706 is comprised of coalescing filter media.
- the coalescer element 706 circumferentially surrounds the spiral vane preseparator 704 .
- Both the spiral vane preseparator 704 and the coalescer element 706 are rotated about a central axis to effect pumping of the blow-by gas through the rotating coalescer 700 and to effect separation of the oil from the blow-by gas.
- the spiral vane preseparator 704 separates the bigger aerosol in the blow-by gas mitigating the risk that the coalescer element 706 becomes plugged with the highly viscous emulsion or soot contained in the blow-by gas. Accordingly, the spiral vane preseparator 704 increases the service life of the coalescer element 706 .
- the spiral vane preseparator 704 and the coalescer element 706 are each coupled to a first endplate 708 and a second endplate 710 .
- the first endplate 708 is solid.
- the second endplate 710 includes the central inlet 702 .
- the first endplate 708 and the second endplate 710 seal the clean side of the rotating coalescer 700 from the dirty side of the rotating coalescer 700 such that the blow-by gas cannot bypass the rotating coalescer 700 .
- the first endplate 708 includes a shroud 712 .
- the shroud 712 guides separated oil exiting the spiral vane preseparator 704 to the second endplate 710 via gravity.
- the shroud 712 circumscribes the spiral vane preseparator 704 .
- the separated oil falls from the shroud and exits a weep hole 714 in the second endplate 710 for drainage from a housing of the rotating coalescer 700 .
- a plurality of weep holes 714 are positioned along the second endplate 710 (e.g., as shown in FIG. 9 ).
- the first endplate 708 is also coupled to a shaft 716 that effects rotation of the rotating coalescer 700 .
- the second endplate includes an oleophobic screen 718 .
- the oleophobic screen 718 circumscribes the spiral vane preseparator 704 .
- the oleophobic screen 718 is an oleophobic media or screen that guides separated oil exiting the spiral vane preseparator 704 to the second endplate 710 via gravity such that the separated oil can exit the weep hole 714 .
- the oleophobic screen allows blow-by gas to pass through the oleophobic screen 718 and into the coalescer element 706 .
- the oleophobic screen 718 is radially offset from the shroud 712 with respect to a center axis of the rotating coalescer 700 such that the oleophobic screen 718 is farther away from the center axis than the shroud 712 (e.g., as shown best in FIG. 9 ).
- the oleophobic screen 718 beads up separated oil and allows the separated oil to drain to the second endplate 710 and out the weep hole 714 .
- the oleophobic screen 718 is in contact with the coalescer element 706 and provides structural support to the coalescer element 706 .
- An axial gap 720 exists between the shroud 712 and the oleophobic screen 718 such that the blow-by gas can pass from the spiral vane preseparator 704 to the coalescer element 706 .
- the gap 720 is sized to minimize the chance that oil droplets separated by the spiral vane preseparator 704 contact the coalescer element 706 .
- FIGS. 8 and 9 cross-sectional views of the endplates 708 and 710 of the rotating coalescer 700 are shown.
- FIG. 8 shows a cross-sectional view showing the first endplate 708 .
- FIG. 9 shows a cross-sectional view showing the second endplate 710 .
- the spiral vane preseparator 704 includes a plurality of vanes 722 .
- Each of the vanes 722 is spaced apart to permit blow-by gas to flow between adjacent vanes.
- Each of the vanes 722 is curved. The curvature of the vanes 722 is selected to create a pumping effect on the blow-by gas when the rotating coalescer 700 is rotating.
- the curvature of the vanes 722 provides an impact surface for oil in the blow-by gas to undergo inertial separation from the air in the blow-by gas.
- separated and coalesced droplets of oil are pushed along the walls of the vanes 722 due to the radial flux of the flow and can either hit the shroud 712 or can drain to the bottom of the second endplate 710 . Draining of the oil out of the weep hole 714 can occur during operation or after the rotating coalescer 700 has stopped rotating or has slowed rotation(e.g., after the engine has shut off).
- FIG. 10 a cross-sectional view of the rotating coalescer 700 fitted within a housing 1002 is shown.
- the first endplate 708 is fitted with a de-swirler 1004 .
- the de-swirler 1004 reduces the rotation of the filtered air exiting the rotating coalescer 700 , which provides a smoother flow of filtered air out of the housing 1002 .
- the filtered air leaving the rotating coalescer 700 is a swirling flow.
- the swirling flow coming out of the rotating coalescer 700 will slow down due to proximity to the stationary wall of the housing 1002 . However, as the swirling flow nears the outlet 1006 of the housing 1002 , the swirling flow will begin spinning faster due to conservation of angular momentum.
- the de-swirler 1004 is configured to reduce the rotational speed of the swirling flow.
- the de-swirler 1004 includes a plurality of vanes 1008 .
- the vanes 1008 are curved in the opposite direction of the vanes 722 of the spiral vane preseparator 704 .
- the vanes 1008 deflect the swirling flow of filtered air in the opposite direction of rotation of the swirling flow thereby reducing the rotational velocity of the filtered air to a small value.
- the straightening of the swirling flow reduces the pressure drop of the rotating coalescer 700 .
- the vanes 1008 provide protection against oil carry over.
- Coupled means the joining of two members directly or indirectly to one another. Such joining may be stationary (e.g., permanent) or movable (e.g., removable or releasable). Such joining may be achieved with the two members or the two members and any additional intermediate members being integrally formed as a single unitary body with one another or with the two members or the two members and any additional intermediate members being attached to one another.
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- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
- Separating Particles In Gases By Inertia (AREA)
Abstract
Description
- The field of the invention relates to coalescing devices. In particular, the field of the invention relates to coalescing devices comprising multiple rotating separation elements.
- Rotating coalescers are utilized in crankcase ventilation (CV) systems for removing oil from crankcase blow-by gases. Typically, the blow-by gases enter the rotating coalescer device axially at the center of the device. The gases are turned 90 degrees, pass through a rotating coalescer section, and exit radially from the outer face of the rotating coalescer device. The rotating coalescer device itself is in the form of a ring and the space in the middle of the ring is either left open or optionally includes radial vanes which facilitate flow through the device.
- Rotating coalescers may include fibrous filters as well as centrifugal separation devices. Performance attributes of rotating coalescer devices may be measured in terms of pressure drop (or rise) through the device and efficiency of oil removal. In rotating coalescers, the oil droplets (e.g., aerosol) suspended and transported by the blow-by gas are separated inside the coalescer media through the particle capture mechanisms of inertial impaction, interception, and diffusion. By rotating the media, inertial impaction is enhanced by the additional centrifugal force. In addition to this aspect, after the oil droplets coalesce to form larger drops, the centrifugal force removes the larger drops by overcoming the surface drag force of the media fibers. This aspect increases the coalescence of the oil from the coalescer by providing improved drainage compared to a stationary coalescer. In turn, the improved drainage from the rotating coalescing filter aids in improving the filtration efficiency as well as greatly reducing the pressure drop across the filter.
- Various embodiments relate to multiple stage rotating coalescer devices that exhibit increased efficiency and reduced pressure drop are described. One stage of the device is a rotating coalescer element. The devices may include an additional separation element, either upstream or downstream of the rotating coalescer element, which may include a cone stack separator or an additional rotating coalescer element.
- One exemplary embodiment relates to a multiple stage rotating coalescer device. The multiple stage rotating coalescer device includes a first stage including a rotating coalescing element. The rotating coalescing element includes coalescing media. The device includes a second stage. The second stage is either upstream or downstream of the first stage. The second stage includes one of a rotating cone stack separator or a separate rotating coalescing element having coalescing media.
- Another exemplary embodiment relates to a rotating coalescer system. The system includes a housing having an inlet and an outlet. The inlet is configured to receive blow-by gas from a crankcase of an internal combustion engine. The outlet is configured to output filtered air. The system further includes a rotating coalescer positioned within the housing. The rotating coalescer includes a first endplate and a second endplate. A spiral vane preseparator is positioned between the first endplate and the second endplate. The spiral vane preseparator includes a plurality of curved vanes that cause separation of an oil from the blow-by gas and pumping of the blow-by gas when the spiral vane preseparator is rotating. The rotating coalescer further includes a coalescer element circumferentially surrounding the spiral vane preseparator and positioned between the first endplate and the second endplate. The coalescer element is comprised of coalescer media. The rotating coalescer includes a de-swirler coupled to the first endplate opposite the spiral vane preseparator and the coalescer element.
- These and other features, together with the organization and manner of operation thereof, will become apparent from the following detailed description when taken in conjunction with the accompanying drawings, wherein like elements have like numerals throughout the several drawings described below.
-
FIG. 1 is a cross-sectional view of a rotating coalescer device according to an exemplary embodiment. -
FIG. 2 is a close-up cross-sectional view of the coalescer device ofFIG. 1 . -
FIG. 3 is a cross-sectional view of a rotating coalescing device according to another exemplary embodiment. -
FIG. 4 is a cross-sectional view of a rotating coalescer device according to still another exemplary embodiment. -
FIG. 5 is a cross-sectional view of a rotating coalescer device according to a further exemplary embodiment. -
FIG. 6 is a cross-sectional view of a rotating coalescer device according to yet another exemplary embodiment. -
FIG. 7 is a cross-sectional perspective view of a rotating coalescer according to an exemplary embodiment. -
FIGS. 8 and 9 are cross-sectional views of the endplates of the rotating coalescer ofFIG. 7 . -
FIG. 10 is a cross-sectional view of the rotating coalescer ofFIG. 7 fitted within a housing and having a de-swirler attached. -
FIG. 11 is a cross-sectional view showing the de-swirler ofFIG. 10 . - Referring to the figures generally, multiple stage rotating coalescer devices are described. The multiple stage rotating coalescing devices exhibit advantages over rotating coalescing devices of the prior art. In some embodiments, the presently disclosed devices may include an integrated coalescing element upstream or downstream of a cone stack centrifugal separator in order to improve efficiency and pumping power of the devices. The devices may include two stages of aerosol separation (e.g., for rotating-type separators). In further embodiments, the presently disclosed devices also may include a shroud that collects and drains collected oil from the interstitial space between the cone stack separator and the coalescing element. In even further embodiments, the devices may integrate a cone stack separator downstream of a coalescing element in an outside-in configuration in order to improve overall performance and better accommodate the air/oil flow through the device.
- In some embodiments, the disclosed devices may include a secondary rotating coalescer element downstream of a primary rotating coalescer element, where flow through the primary rotating element is inside-out and flow through the secondary rotating element is outside-in. The two rotating elements may share the same base plate. The primary and secondary elements rotate on single-drive or multiple-drive mechanisms that utilize single or multiple shafts and have multiple seals. The rotation of the primary and secondary element in the presently disclosed devices may provide continuous self-cleaning of the media of the elements and enhanced droplet coalescing. The fiber architecture of the media of the primary and secondary elements may be the same or different and optionally may include oleophobic treatment. For example, the media of the secondary element may be an oleophobic screen that prevents oil carryover and increases the pumping effect of the device.
- Referring to
FIG. 1 , a cross-sectional view of a rotatingcoalescer device 100 is shown according to an exemplary embodiment. Thecoalescer device 100 includes a centrifugalcone stack separator 102 positioned in the center of thecoalescer device 100. Thecone stack separator 102 acts as a pre-cleaner, providing an initial stage of inertial separation of aerosol (e.g., oil) from blow-by gases entering theinlet 104 prior to the blow-by gases passing through the coalescingelement 106. The coalescingelement 106 is comprised of a coalescing media. The coalescingelement 106 is a second stage of separation of aerosol from the blow-by gases. The pre-cleaning reduces the total amount of oil that the coalescingelement 106 needs to separate by pre-capturing some fraction of the overall oil aerosol contained in the crankcase blow-by gases. Thecone stack separator 102 also increases the amount of pumping of the blow-by gas flow in thecoalescer device 100. In addition, thecone stack separator 102 also helps to distribute the flow evenly across the inlet face of the coalescingelement 106 thereby increasing the performance of the coalescingelement 106. - During operation of the
coalescer device 100, both thecone stack separator 102 and the coalescingelement 106 are coupled to and rotated by ashaft 108 passing through the center of thecoalescer device 100. In some arrangements, theshaft 108 is hollow and provides the inlet into thecoalescer device 100. The blow-by gas flow enters the center of ahousing 110 of thedevice 100, into the inside of thecone stack separator 102 via theinlet 104. Within thecone stack separator 102, blow-by gas flows radially outward where at least some of the aerosol in the blow-by gas is removed due to centrifugal impaction of the aerosol on the surfaces of thecone stack separator 102. Thecone stack separator 102 further adds mechanical energy to the blow-by gas flow by accelerating the flow of the blow-by gas in a tangential direction with respect to the center axis of thecoalescer device 100. The added mechanical energy to the blow-by gas by thecone stack separator 102 creates a pumping effect similar to the action of a pump, which reduces the pressure drop caused by thecoalescer device 100. After exiting from thecone stack separator 102, the blow-by gas flow enters the coalescingelement 106 where additional filtration (e.g., coalescing of the aerosol in the blow-by gas) and pumping takes place. Upon leaving thecoalescer device 100, the blow-by flow is vented either to the atmosphere (e.g., as done in an open CV system) or back to an intake stream (e.g., to the turbocharger inlet) of the internal combustion engine for combustion (e.g., as done in a closed CV system). - Referring to
FIG. 2 , a close-up cross-sectional view of thecoalescer device 100 is shown.FIG. 2 shows the flow of the blow-by gas passing through thecone stack separator 102 and through the coalescingelement 106. As shown inFIG. 2 , thecone stack separator 102 is comprised of a plurality ofcones 202. Thecones 202 are spaced out to provide a plurality of flow paths in between pairs ofadjacent cones 202. Each of thecones 202 includes a bend that causes the centrifugal impaction of the aerosol on the surfaces of thecone stack separator 102 as discussed above. -
FIG. 3 shows a cross-sectional view of acoalescer device 300 is shown according to an exemplary embodiment. Thecoalescer device 300 is a rotating coalescer device. Similar to thecoalescer device 100, thecoalescer device 300 includes acone stack separator 302 and a coalescingelement 304 comprised of coalescing media. Thecone stack separator 302 and the coalescing media are housed within ahousing 306. During operation, thecone stack separator 302 and the coalescingelement 304 are rotated about acentral axis 308 in a similar manner as described above with respect to thecoalescer device 100. Thecoalescer device 300 separatesoil 310 from aflow 312 of blow-by gases containing aerosol. In some arrangements, thecones 314 of the cone stack separator include spacers (e.g., raised ridges, ribs, dots, etc.) that radiate out in a straight line or a curve. These spacers provide separation between thecones 314. Thecoalescer device 300 includes ashroud 316 that collectsoil 310 exiting from thecone stack separator 302. The collectedoil 310 falls down the face of the shroud to the bottom of therotating module 318 due to gravity. Therotating module 318 housescone stack separator 302 and the coalescingelement 304 for rotation within thehousing 306. The open area below theshroud 316 leading to thecoalescer element 304 is arranged such that the collectedoil 310 is not carried over to thecoalescer element 304 and instead collects at the bottom of therotating module 318 where it drains through apreseparator drain 320. Thepreseparator drain 320 rotates with therotating module 318. Thepreseparator drain 320 is sized and positioned based on the pressure difference on either side of therotating module 318 to allow for draining of the separatedoil 310 via gravity. The dimensions of thepreseparator drain 320 are selected in order to minimize the potential for blow-by gas flow from thecone stack separator 302 to bypass thecoalescer element 304 by flowing out of thepreseparator drain 320. The size of thepreseparator drain 320 is also sized based at least in part on the pumping force generated by thecone stack separator 302.Separated oil 310 does not flow back through the inlet because therotating module 318 is sealed against thehousing 310 through at least one seal 322 (shown as two seals).Oil 310 separated via thecone stack separator 302 and thecoalescer element 304 is drained from the housing via ahousing drain 324. -
FIG. 4 shows a cross-sectional view of acoalescing device 400 according to an exemplary embodiment. The coalescingdevice 400 includes acone stack separator 402, which functions as an inertial post-separator, and arotating coalescer element 404 comprised of coalescing media. Thecone stack separator 402 functions as an inertial post-separator because thecone stack separator 402 is positioned downstream of therotating coalescer element 404 with respect to the by-pass gas flow 406. Thecone stack separator 402 and the coalescingelement 404 are rotated in a similar manner as described above with respect todevices pass gas flow 406. In thecoalescing device 400, a top portion of the coalescing element opposite theinlet 408 is received in a bottom portion of thecone stack separator 402, which is utilized for guidingoil 410 to thedrain 412 of thehousing 414. In thecoalescing device 400, slots or holes may be provided to improve drainage and prevent oil carryover. -
FIG. 5 shows a cross-sectional view of arotating coalescer device 500 according to another exemplary embodiment. Therotating coalescer device 500 includes a cone stack separator 502 placed downstream of acoalescer element 504 in an inside-out flow configuration. Thecoalescer device 500 ofFIG. 5 is designed to reduce oil carryover and to separate out re-entrained droplets. Thecoalescer device 500 may be particularly desirable for coalescers having a housing that is diametrically constrained (e.g., due to limited space on an engine-mounted device), where oil carryover is particularly an issue. In therotating coalescer device 500, the post-separator cone stack separator 502 has inside-out flow and the re-entrained oil is flung from the device due to centrifugal force. Separated oil drains from the housing 506 through adrain 508. The cone stack separator 502 is shaped to direct the flow of blow-by gas towards thedrain 508. The cone stack separator 502 includes slots orholes 510 to drain the coalesced droplets by gravitational force and by positive pumping pressure created through the rotation of thecoalescer element 504 and the cone stack separator 502. The media of thecoalescer element 504 may be embedded or coupled to the cone stack separator 502. - Referring to
FIG. 6 , a cross-sectional view of arotating coalescer device 600 is shown according to another exemplary embodiment. Therotating coalescer device 600 includes a primaryrotating coalescing element 602 and a downstream, secondaryrotating coalescing element 604. Both the primary and secondaryrotating coalescing elements rotating coalescer device 600. Both the primary and secondaryrotating coalescing elements secondary element 604 can be comprised of either similar filter media material or another type of media material as theprimary coalescing element 602. The two coalescingelements barrier 606 positioned between the twoelements barrier 606 ensures that by-pass gas flows first through the primary coalescing element 602 (in an inside-out flow pattern) and then through the secondary coalescing element 604 (in an outside-in flow pattern). Thebarrier 606 ensures that the by-pass gases flowing through the two coalescingelements secondary coalescing elements inlet 608 on the upstream side and then exits radially out of theprimary coalescing element 602. The flow then passes through a secondaryrotating coalescing element 604 on its way towards the downstream clean side. As the by-pass gas flows through thesecondary coalescing element 604, thesecondary coalescing element 604 captures any re-entrained oil droplets and excessive oil that gets carried over rendering the air flow on the downstream side completely oil free. Thesecondary coalescing element 604 will eliminate any carryover oil that has not previously drained from the device. Any further carryover oil has to overcome the centrifugal force created by the rotating secondary element. Clean air passes out of thehousing 610 through anoutlet 612. Separated oil exits the housing through adrain 614. - Referring to
FIG. 7 , a cross-sectional perspective view of arotating coalescer 700 is shown according to still another exemplary embodiment. Therotating coalescer 700 separates oil from blow-by gas entering therotating coalescer 700 through acentral inlet 702. Therotating coalescer 700 is a two-stage coalescer. The blow-by gas is first routed from thecentral inlet 702 through aspiral vane preseparator 704 in an inside-out flow direction. After passing through thespiral vane preseparator 704, the blow-by gas is routed through acoalescer element 706. Thecoalescer element 706 is comprised of coalescing filter media. Thecoalescer element 706 circumferentially surrounds thespiral vane preseparator 704. Both thespiral vane preseparator 704 and thecoalescer element 706 are rotated about a central axis to effect pumping of the blow-by gas through therotating coalescer 700 and to effect separation of the oil from the blow-by gas. Thespiral vane preseparator 704 separates the bigger aerosol in the blow-by gas mitigating the risk that thecoalescer element 706 becomes plugged with the highly viscous emulsion or soot contained in the blow-by gas. Accordingly, thespiral vane preseparator 704 increases the service life of thecoalescer element 706. - The
spiral vane preseparator 704 and thecoalescer element 706 are each coupled to afirst endplate 708 and asecond endplate 710. Thefirst endplate 708 is solid. Thesecond endplate 710 includes thecentral inlet 702. Thefirst endplate 708 and thesecond endplate 710 seal the clean side of therotating coalescer 700 from the dirty side of therotating coalescer 700 such that the blow-by gas cannot bypass therotating coalescer 700. Thefirst endplate 708 includes ashroud 712. Theshroud 712 guides separated oil exiting thespiral vane preseparator 704 to thesecond endplate 710 via gravity. Theshroud 712 circumscribes thespiral vane preseparator 704. The separated oil falls from the shroud and exits a weephole 714 in thesecond endplate 710 for drainage from a housing of therotating coalescer 700. In some arrangements, a plurality of weepholes 714 are positioned along the second endplate 710 (e.g., as shown inFIG. 9 ). Thefirst endplate 708 is also coupled to ashaft 716 that effects rotation of therotating coalescer 700. The second endplate includes anoleophobic screen 718. Theoleophobic screen 718 circumscribes thespiral vane preseparator 704. Theoleophobic screen 718 is an oleophobic media or screen that guides separated oil exiting thespiral vane preseparator 704 to thesecond endplate 710 via gravity such that the separated oil can exit the weephole 714. The oleophobic screen allows blow-by gas to pass through theoleophobic screen 718 and into thecoalescer element 706. Theoleophobic screen 718 is radially offset from theshroud 712 with respect to a center axis of therotating coalescer 700 such that theoleophobic screen 718 is farther away from the center axis than the shroud 712 (e.g., as shown best inFIG. 9 ). Theoleophobic screen 718 beads up separated oil and allows the separated oil to drain to thesecond endplate 710 and out the weephole 714. In some arrangements, theoleophobic screen 718 is in contact with thecoalescer element 706 and provides structural support to thecoalescer element 706. Anaxial gap 720 exists between theshroud 712 and theoleophobic screen 718 such that the blow-by gas can pass from thespiral vane preseparator 704 to thecoalescer element 706. Thegap 720 is sized to minimize the chance that oil droplets separated by thespiral vane preseparator 704 contact thecoalescer element 706. - Referring to
FIGS. 8 and 9 , cross-sectional views of theendplates rotating coalescer 700 are shown.FIG. 8 shows a cross-sectional view showing thefirst endplate 708.FIG. 9 shows a cross-sectional view showing thesecond endplate 710. As shown inFIGS. 8 and 9 , thespiral vane preseparator 704 includes a plurality ofvanes 722. Each of thevanes 722 is spaced apart to permit blow-by gas to flow between adjacent vanes. Each of thevanes 722 is curved. The curvature of thevanes 722 is selected to create a pumping effect on the blow-by gas when therotating coalescer 700 is rotating. Additionally, the curvature of thevanes 722 provides an impact surface for oil in the blow-by gas to undergo inertial separation from the air in the blow-by gas. During operation, separated and coalesced droplets of oil are pushed along the walls of thevanes 722 due to the radial flux of the flow and can either hit theshroud 712 or can drain to the bottom of thesecond endplate 710. Draining of the oil out of the weephole 714 can occur during operation or after therotating coalescer 700 has stopped rotating or has slowed rotation(e.g., after the engine has shut off). - Referring to
FIG. 10 , a cross-sectional view of therotating coalescer 700 fitted within ahousing 1002 is shown. In the arrangement ofFIG. 10 , thefirst endplate 708 is fitted with a de-swirler 1004. The de-swirler 1004 reduces the rotation of the filtered air exiting therotating coalescer 700, which provides a smoother flow of filtered air out of thehousing 1002. The filtered air leaving therotating coalescer 700 is a swirling flow. The swirling flow coming out of therotating coalescer 700 will slow down due to proximity to the stationary wall of thehousing 1002. However, as the swirling flow nears theoutlet 1006 of thehousing 1002, the swirling flow will begin spinning faster due to conservation of angular momentum. Accordingly, the swirling flow will reach the rotational speed of therotating coalescer 700 at some radial location along thefirst endplate 708 if not stopped. Accordingly, the de-swirler 1004 is configured to reduce the rotational speed of the swirling flow. As shown inFIG. 11 , the de-swirler 1004 includes a plurality ofvanes 1008. Thevanes 1008 are curved in the opposite direction of thevanes 722 of thespiral vane preseparator 704. Thevanes 1008 deflect the swirling flow of filtered air in the opposite direction of rotation of the swirling flow thereby reducing the rotational velocity of the filtered air to a small value. The straightening of the swirling flow reduces the pressure drop of therotating coalescer 700. Additionally, thevanes 1008 provide protection against oil carry over. - In the foregoing description, certain terms have been used for brevity, clearness, and understanding. No unnecessary limitations are to be implied therefrom beyond the requirement of the prior art because such terms are used for descriptive purposes and are intended to be broadly construed. The different configurations, systems and method steps described herein may be used alone or in combination with other configurations, systems and method steps. It is to be expected that various equivalents, alternatives and modifications are possible.
- It should be noted that any use of the term “exemplary” herein to describe various embodiments is intended to indicate that such embodiments are possible examples, representations, and/or illustrations of possible embodiments (and such term is not intended to connote that such embodiments are necessarily extraordinary or superlative examples).
- The terms “coupled” and the like as used herein mean the joining of two members directly or indirectly to one another. Such joining may be stationary (e.g., permanent) or movable (e.g., removable or releasable). Such joining may be achieved with the two members or the two members and any additional intermediate members being integrally formed as a single unitary body with one another or with the two members or the two members and any additional intermediate members being attached to one another.
- References herein to the positions of elements (e.g., “top,” “bottom,” “above,” “below,” etc.) are merely used to describe the orientation of various elements in the FIGURES. It should be noted that the orientation of various elements may differ according to other exemplary embodiments, and that such variations are intended to be encompassed by the present disclosure.
- It is important to note that the construction and arrangement of the various exemplary embodiments are illustrative only. Although only a few embodiments have been described in detail in this disclosure, those skilled in the art who review this disclosure will readily appreciate that many modifications are possible (e.g., variations in sizes, dimensions, structures, shapes and proportions of the various elements, values of parameters, mounting arrangements, use of materials, colors, orientations, etc.) without materially departing from the novel teachings and advantages of the subject matter described herein. For example, elements shown as integrally formed may be constructed of multiple parts or elements, the position of elements may be reversed or otherwise varied, and the nature or number of discrete elements or positions may be altered or varied. The order or sequence of any process or method steps may be varied or re-sequenced according to alternative embodiments, and elements from different embodiments may be combined in a manner understood to one of ordinary skill in the art. Other substitutions, modifications, changes and omissions may also be made in the design, operating conditions and arrangement of the various exemplary embodiments without departing from the scope of the present invention.
Claims (42)
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US10537842B2 (en) | 2015-06-09 | 2020-01-21 | Cummins Filtration Ip, Inc. | Systems and methods for utilizing a low-friction rotating coalescer contact seal |
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US10682601B2 (en) | 2015-08-28 | 2020-06-16 | Cummins Filtration Ip, Inc. | Rotating coalescing element with directed liquid drainage and gas outlet |
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Citations (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3362155A (en) * | 1965-03-29 | 1968-01-09 | Gen Electric | Axial flow separator |
US6033450A (en) * | 1995-12-21 | 2000-03-07 | United Technologies Corporation | Deoiler shaft vortex separator |
US6183407B1 (en) * | 1998-04-02 | 2001-02-06 | Alfa Laval Ab | Centrifugal separator having axially-extending, angled separation discs |
US6499285B1 (en) * | 2001-08-01 | 2002-12-31 | Rolls-Royce Corporation | Particle separator for a gas turbine engine |
US6652439B2 (en) * | 2000-04-04 | 2003-11-25 | Fleetguard, Inc. | Disposable rotor shell with integral molded spiral vanes |
US20040214710A1 (en) * | 2003-04-23 | 2004-10-28 | Herman Peter K. | Integral air/oil coalescer for a centrifuge |
US20070175191A1 (en) * | 2006-01-27 | 2007-08-02 | Mecs, Inc. | Fiber Bed assembly and fiber bed therefor |
US20090000258A1 (en) * | 2006-02-13 | 2009-01-01 | Alfa Laval Corporate Ab | Centrifugal Separator |
US20090067986A1 (en) * | 2007-03-26 | 2009-03-12 | Honeywell International, Inc. | Vortex spoiler for delivery of cooling airflow in a turbine engine |
US20090101013A1 (en) * | 2007-10-23 | 2009-04-23 | Moredock James G | Powered air cleaning system and air cleaning method |
US20090263238A1 (en) * | 2008-04-17 | 2009-10-22 | Minebea Co., Ltd. | Ducted fan with inlet vanes and deswirl vanes |
US20100229511A1 (en) * | 2007-10-02 | 2010-09-16 | Mann+Hummel Gmbh | Filter Element Having Serrated Seal |
US20110180051A1 (en) * | 2010-01-27 | 2011-07-28 | Cummins Filtration Ip Inc. | Crankcase Ventilation Inside-Out Flow Rotating Coalescer |
US20110247309A1 (en) * | 2010-01-27 | 2011-10-13 | Cummins Filtration Ip Inc. | Magnetically Driven Rotating Separator |
US20120034083A1 (en) * | 2010-08-06 | 2012-02-09 | Minebea Co., Ltd. (Minebea) | Fan with area expansion between rotor and stator blades |
US20140069432A1 (en) * | 2011-04-18 | 2014-03-13 | Resmed Motor Technology Inc. | Pap system blower |
US20140096683A1 (en) * | 2012-10-04 | 2014-04-10 | Mecs, Inc. | Fiber bed assembly including a re-entrainment control device for a fiber bed mist eliminator |
US20150075377A1 (en) * | 2012-05-29 | 2015-03-19 | Elringklinger Ag | Separator and method for separating liquid droplets from an aerosol |
US20150173577A1 (en) * | 2013-12-24 | 2015-06-25 | Samsung Electronics Co., Ltd. | Cleaning device |
US20160245157A1 (en) * | 2015-02-25 | 2016-08-25 | Honeywell International Inc. | Wastegate with injected flow |
Family Cites Families (48)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1941194U (en) | 1966-03-23 | 1966-06-23 | Draftex G M B H | SEALING OR DECORATIVE STRIP SLIDED ON A FLANGE. |
JPS5392973A (en) | 1977-01-26 | 1978-08-15 | Sanetsu Kk | Oil mist remover |
US4482365A (en) | 1982-03-01 | 1984-11-13 | Pall Corporation | Vortex air cleaner and self-cleaning barrier filter assembly for supercharged engines |
US4487618A (en) | 1982-08-19 | 1984-12-11 | La-Man Corporation | Airline vapor trap |
US4516994A (en) | 1984-04-11 | 1985-05-14 | Vilter Manufacturing Corporation | Apparatus for separating liquid droplets from gas |
US4514193A (en) | 1984-07-26 | 1985-04-30 | Donaldson Company, Inc. | Self-cleaning air cleaner assembly with rotating filter element and inertial pre-cleaner |
DE3737221C1 (en) | 1987-11-03 | 1989-04-27 | Mtu Muenchen Gmbh | OEl air separator |
US5056935A (en) | 1990-11-05 | 1991-10-15 | General Electric Company | Oil film damper seal ring |
US5387342A (en) | 1992-06-10 | 1995-02-07 | Charles W. Taggart | Centrifugal separator and method |
GB9320231D0 (en) | 1993-10-01 | 1993-11-17 | Boc Group Plc | Gas-liquid separation methods and apparatus |
US5716423A (en) | 1995-12-21 | 1998-02-10 | United Technologies Corporation | Multi-stage deoiler with porous media |
US6123061A (en) | 1997-02-25 | 2000-09-26 | Cummins Engine Company, Inc. | Crankcase ventilation system |
JPH11141325A (en) | 1997-11-11 | 1999-05-25 | Toyota Autom Loom Works Ltd | Oil reflux device for blowby gas |
US6139595A (en) | 1998-09-18 | 2000-10-31 | Fleetguard, Inc. | Air/oil coalescer with centrifugally assisted drainage |
SE516944C2 (en) | 1999-06-30 | 2002-03-26 | Volvo Lastvagnar Ab | Oil separator for small particles |
DE10044615A1 (en) | 2000-09-09 | 2002-04-04 | Mahle Filtersysteme Gmbh | Ventilation device for a crankcase |
US6640792B2 (en) | 2001-08-16 | 2003-11-04 | Commins Engine Company, Inc. | Air/oil coalescer with an improved centrifugally assisted drainage |
US6517612B1 (en) | 2001-10-29 | 2003-02-11 | Gore Enterprise Holdings, Inc. | Centrifugal filtration device |
SE0201982D0 (en) | 2002-06-24 | 2002-06-24 | Alfa Laval Corp Ab | Ways to clean crankcase gas and a gas purifier separator |
DE20302824U1 (en) | 2003-02-21 | 2004-07-08 | Hengst Gmbh & Co.Kg | Oil separator for cleaning crankcase ventilation gas of an internal combustion engine containing oil mist |
GB0417458D0 (en) | 2004-08-05 | 2004-09-08 | Domnick Hunter Ltd | Filter assembly |
EP1645320A1 (en) | 2004-10-08 | 2006-04-12 | Mann+Hummel Gmbh | Centrifugal separator |
KR101514908B1 (en) | 2004-11-05 | 2015-04-23 | 도날드슨 컴파니, 인코포레이티드 | Filter medium and structure |
US8057567B2 (en) | 2004-11-05 | 2011-11-15 | Donaldson Company, Inc. | Filter medium and breather filter structure |
DE102005021278B4 (en) | 2005-05-09 | 2010-04-15 | Alfa Laval Tumba Ab | Device for cleaning gas when venting a crankcase |
SE529611C2 (en) | 2006-02-13 | 2007-10-02 | Alfa Laval Corp Ab | centrifugal |
SE529610C2 (en) | 2006-02-13 | 2007-10-02 | Alfa Laval Corp Ab | centrifugal |
US7338546B2 (en) * | 2006-04-19 | 2008-03-04 | Alfa Laval Corporate Ab | Centrifugal separator for cleaning gas generated by an internal combustion engine and a method for operating the same |
DE102006024816A1 (en) | 2006-05-29 | 2007-12-06 | Mahle International Gmbh | Device for venting a crankcase |
WO2008103736A1 (en) | 2007-02-22 | 2008-08-28 | Donaldson Company, Inc. | Filter element and method |
DE202007009913U1 (en) | 2007-07-13 | 2008-11-20 | Hengst Gmbh & Co.Kg | Separator for separating oil mist from the crankcase ventilation gas of an internal combustion engine and internal combustion engine with a separator |
US7708793B2 (en) | 2007-08-29 | 2010-05-04 | Bendix Commercial Vehicle Systems Llc | Purge exhaust processor |
DE102008005574B4 (en) | 2008-01-22 | 2013-11-28 | Areva Gmbh | centrifugal |
FR2933626B1 (en) | 2008-07-10 | 2011-01-21 | Filtrauto | DEVICE WITH ROTOR WITH MEDIA COALESCER FOR SEPARATING THE OIL FROM THE CASING GASES OF AN INTERNAL COMBUSTION ENGINE. |
US8069658B2 (en) | 2008-11-26 | 2011-12-06 | Corning Incorporated | Methods for estimating particulate load in a particulate filter, and related systems |
US8974567B2 (en) | 2010-01-27 | 2015-03-10 | Cummins Filtration Ip Inc. | Rotating coalescer with keyed drive |
US8893689B2 (en) | 2010-01-27 | 2014-11-25 | Cummins Filtration Ip, Inc. | Crankcase ventilation self-cleaning coalescer with intermittent rotation |
US9056268B2 (en) | 2010-02-12 | 2015-06-16 | Donaldson Company, Inc. | Liquid filtration media, filter elements and methods |
WO2011106205A2 (en) | 2010-02-23 | 2011-09-01 | 3M Innovative Properties Company | Dimensionally stable nonwoven fibrous webs and methods of making and using the same |
EP2561127B1 (en) | 2010-04-22 | 2015-01-21 | 3M Innovative Properties Company | Nonwoven nanofiber webs containing chemically active particulates and methods of making and using same |
EP2670507B1 (en) | 2011-02-03 | 2021-06-30 | Donaldson Company, Inc. | Filter media pack, filter assembly, and method |
WO2013025445A2 (en) | 2011-08-12 | 2013-02-21 | Donaldson Company, Inc. | Liquid filtration media containing melt-blown fibers |
BR112014009743A2 (en) | 2011-11-04 | 2017-05-02 | Cummins Filtration Ip Inc | rotary separator for separating fluid from fluid mix |
WO2016046944A1 (en) | 2014-09-25 | 2016-03-31 | 東京濾器株式会社 | Separation disk for oil separator, rotor for oil separator, and oil separator |
DE102015202946A1 (en) | 2015-02-18 | 2016-08-18 | Mahle International Gmbh | Pumping device for driving blow-by gas |
US10543442B2 (en) | 2015-03-30 | 2020-01-28 | Cummins Filtration Ip, Inc. | Multiple stage rotating coalescer devices |
WO2017189516A1 (en) | 2016-04-28 | 2017-11-02 | Cummins Filtration Ip, Inc. | Inside-out rotating coalescer with gas exit through hollow shaft |
DE102016211776A1 (en) | 2016-06-29 | 2018-01-04 | Elringklinger Ag | separating |
-
2015
- 2015-03-30 US US15/561,170 patent/US10543442B2/en active Active
- 2015-03-30 CN CN201580078403.0A patent/CN107405556B/en active Active
- 2015-03-30 DE DE112015006228.9T patent/DE112015006228T5/en not_active Withdrawn
- 2015-03-30 WO PCT/US2015/023290 patent/WO2016159951A1/en active Application Filing
Patent Citations (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3362155A (en) * | 1965-03-29 | 1968-01-09 | Gen Electric | Axial flow separator |
US6033450A (en) * | 1995-12-21 | 2000-03-07 | United Technologies Corporation | Deoiler shaft vortex separator |
US6183407B1 (en) * | 1998-04-02 | 2001-02-06 | Alfa Laval Ab | Centrifugal separator having axially-extending, angled separation discs |
US6652439B2 (en) * | 2000-04-04 | 2003-11-25 | Fleetguard, Inc. | Disposable rotor shell with integral molded spiral vanes |
US6499285B1 (en) * | 2001-08-01 | 2002-12-31 | Rolls-Royce Corporation | Particle separator for a gas turbine engine |
US20040214710A1 (en) * | 2003-04-23 | 2004-10-28 | Herman Peter K. | Integral air/oil coalescer for a centrifuge |
US20070175191A1 (en) * | 2006-01-27 | 2007-08-02 | Mecs, Inc. | Fiber Bed assembly and fiber bed therefor |
US20090000258A1 (en) * | 2006-02-13 | 2009-01-01 | Alfa Laval Corporate Ab | Centrifugal Separator |
US20090067986A1 (en) * | 2007-03-26 | 2009-03-12 | Honeywell International, Inc. | Vortex spoiler for delivery of cooling airflow in a turbine engine |
US20100229511A1 (en) * | 2007-10-02 | 2010-09-16 | Mann+Hummel Gmbh | Filter Element Having Serrated Seal |
US20090101013A1 (en) * | 2007-10-23 | 2009-04-23 | Moredock James G | Powered air cleaning system and air cleaning method |
US20090263238A1 (en) * | 2008-04-17 | 2009-10-22 | Minebea Co., Ltd. | Ducted fan with inlet vanes and deswirl vanes |
US20110180051A1 (en) * | 2010-01-27 | 2011-07-28 | Cummins Filtration Ip Inc. | Crankcase Ventilation Inside-Out Flow Rotating Coalescer |
US20110247309A1 (en) * | 2010-01-27 | 2011-10-13 | Cummins Filtration Ip Inc. | Magnetically Driven Rotating Separator |
US20120034083A1 (en) * | 2010-08-06 | 2012-02-09 | Minebea Co., Ltd. (Minebea) | Fan with area expansion between rotor and stator blades |
US20140069432A1 (en) * | 2011-04-18 | 2014-03-13 | Resmed Motor Technology Inc. | Pap system blower |
US20150075377A1 (en) * | 2012-05-29 | 2015-03-19 | Elringklinger Ag | Separator and method for separating liquid droplets from an aerosol |
US20140096683A1 (en) * | 2012-10-04 | 2014-04-10 | Mecs, Inc. | Fiber bed assembly including a re-entrainment control device for a fiber bed mist eliminator |
US20150173577A1 (en) * | 2013-12-24 | 2015-06-25 | Samsung Electronics Co., Ltd. | Cleaning device |
US20160245157A1 (en) * | 2015-02-25 | 2016-08-25 | Honeywell International Inc. | Wastegate with injected flow |
Cited By (24)
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---|---|---|---|---|
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US10537842B2 (en) | 2015-06-09 | 2020-01-21 | Cummins Filtration Ip, Inc. | Systems and methods for utilizing a low-friction rotating coalescer contact seal |
US11918948B2 (en) | 2015-06-09 | 2024-03-05 | Cummins Filtration Ip, Inc. | Systems and methods for rotating coalescers maintaining positive recirculation through a dynamic seal |
US10436066B2 (en) * | 2015-06-29 | 2019-10-08 | Rolls-Royce Plc | De-oiler and a method of using the same |
US20160376922A1 (en) * | 2015-06-29 | 2016-12-29 | Rolls-Royce Plc | De-oiler and a method of using the same |
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US11504665B2 (en) | 2015-08-28 | 2022-11-22 | Cummins Filtration Ip, Inc. | Rotating coalescing element with directed liquid drainage and gas outlet |
US11156137B2 (en) | 2016-04-28 | 2021-10-26 | Cummins Filtration Ip, Inc. | Inside-out rotating coalescer with gas exit through hollow shaft |
US11448107B2 (en) | 2016-04-28 | 2022-09-20 | Cummins Filtration Ip, Inc. | Inside-out rotating coalescer with gas exit through hollow shaft |
US10927730B2 (en) | 2016-04-28 | 2021-02-23 | Cummins Filtration Ip, Inc. | Inside-out rotating coalescer with gas exit through hollow shaft |
US10711669B2 (en) | 2016-04-28 | 2020-07-14 | Cummins Filtration Ip, Inc. | Inside-out rotating coalescer with gas exit through hollow shaft |
US11173440B2 (en) * | 2016-12-09 | 2021-11-16 | Cummins Filtration Ip, Inc. | Centrifugal separator with improved volumetric surface area packing density and separation performance |
JP2022515395A (en) * | 2018-12-17 | 2022-02-18 | 蘇州市格美納電器有限公司 | Separator and vacuum cleaner with this separator |
US12023619B2 (en) | 2019-02-04 | 2024-07-02 | Cummins Filtration Ip, Inc. | Split flow axial crankcase separator |
US20220249995A1 (en) * | 2019-05-24 | 2022-08-11 | Safran Helicopter Engines | Component for a turbomachine centrifugal degasser with adapted longitudinal walls |
US11925888B2 (en) * | 2019-05-24 | 2024-03-12 | Safran Helicopter Engines | Component for a turbomachine centrifugal degasser with adapted longitudinal walls |
US11759736B2 (en) | 2019-08-30 | 2023-09-19 | Paragon Space Development Corporation | Two-phase separator device for removing condensate or particulate from a gas stream |
US11433337B2 (en) * | 2019-08-30 | 2022-09-06 | Paragon Space Development Corporation | Two-phase separator device for removing condensate or particulate from a gas stream |
US20230085051A1 (en) * | 2020-01-28 | 2023-03-16 | Cummins Filtration Inc. | Electric motor integrated rotating crankcase ventilation filter assemblies |
US11988121B2 (en) * | 2020-01-28 | 2024-05-21 | Cummins Filtration Inc. | Electric motor integrated rotating crankcase ventilation filter assemblies |
CN114917688A (en) * | 2021-02-03 | 2022-08-19 | 中国石油天然气集团有限公司 | Centrifugal separation system |
Also Published As
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DE112015006228T5 (en) | 2017-11-09 |
WO2016159951A1 (en) | 2016-10-06 |
CN107405556A (en) | 2017-11-28 |
US10543442B2 (en) | 2020-01-28 |
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